STARPAK-5B1-XTS-1 Iridium and GPS Dual Mode Antenna, Helix Tail Fin

STARPAK-5B1-XTS-1
Antenna Design: Helix
Profile: commonly referred to as Fin, Tail Fin or Blade shape/style
Mounting Profile
SAT Connector: Base Exit, TNC-Male
GPS Connector: Base Exit, SMA-Female
Mounting: Flat fixed Mount, with “O” Ring gasket and 4x 10-32 Stainless Steel Mounting Screws Supplied

Mechanical
Height: 128.65mm(5.065in)
Length: 133.35(5.25in)
Width: 52.72(2.075in)
Weight: 342g(12.0oz).
Material: 6061-T6 Aluminum Alloy base, Composite Radome, Impact, Abrasion, UV, Solvent, and Fire Retardant
Finish: Skydrol Resistant Polyurethane Enamel Base Iridite PER/ MIL-C-5441F

Environmental
Extreme Low to very High Temperature Operating Range -55° to +85°C (-67° to +185°F)
Altitude: 21.336m(70,000ft)
Vibration: 30 G’s
Leakage: Hermetically Sealed

IRIDIUM TECHNICAL SPECIFICATIONS
Frequency: 1609 – 1626MHz
Radiation Pattern: Hemispherical
Polarization: RHCP
VSWR: <1.5:1
Impedance: 50ohms
Gain(bBlc)
……………………..Free Space…-…4ft G.P.
@ 90° (ZENITH)………….+0.1…-…+1.1
@ 10°………………………..-1.6..-…..-0.8
@ 20°……………………….+0.8..-…..+1.2
@ 30°………………………..-0.7..-…..+1.1
@ 60-90°……………………-0.7..-……0.0
BEAM WIDTH(3dB)…180Deg..-…162Deg
Axial Ratio @ Zenith: 2dB
Power Handling: 3W
Lightning Protection: DC Grounding

L1 GPS TECHNICAL SPECIFICATIONS
Frequency: (1575.42 ± 15) MHz
Radiation Pattern: Hemispherical
Polarization: RHCP
VSWR: <1.5:1 Impedance: 50ohms Gain(bBlc) ……………………….Free Space. -.. 4ft G.P. @ 90° (ZENITH) -………..+4.6…-.+2.9 @ 10°……………..-………..-2.5…-.-1.8 @ 20°……………. -………..-1.1…-.-0.7 @ 30°……………. -………..-0.5…-.+1.7 @ 60-90°…………-…….> .3.6…-..+2.1
BEAM WIDTH(3dB)……103Deg.-..146Deg
Axial Ratio: 2dB
Power Handling: 1W
Lightning Protection: DC Grounding

LNA OPTION FOR GPS
LNA Noise Figure: 33dB Gain
LNA P1dB Out: 3.0dB
LNA DC Power: 2.5V/20mA, 3V/29mA, 3.3V/35mA,(2.5-24)V/<50mA
Rejection @(-50/+50)MHz: -40dB / -40dB
Rejection @(-100/+100)MHz: <-65dB
Power Handling: 50Watts CW(without LNA), 1Watt CW(with LNA)

Network, USA Federal, and Military Specifications
Manufactured in USA
Compatible with Iridium and GPS L1 Satellite Networks.
DO-160D, DO-228, MIL-C-5541
MIL-E-5400, MIL-I-45208A, MIL-STD-810 and SAEJ1455
Acceptance Test Procedure: ATP-GPS-L1L2-100

MANUFACTURER COMPLIANCE
1) ISO 9001-2008: Registered through SGS
2) TSO C-144: Registered through FAA
3) Environmental: TCA/DO-160D, TSO C144
4) Lightning: DO-160F, Direct Effects, Section 23
5) Electrical: TSO C144, RTCA/DO-228/DO-254, Mil-STD-461F
6) CE: EMC Directive 89/336/EEC European Union) & 47CFR, Part 15, Subpart B (FCC)
7) EMC.Emission: EUROPEAN STANDARD EN 55022: 2006 / UNITED STATES STANDARD 47 CFR PART 15, SUBPART B
8) Immunity: EUROPEAN STANDARD EN 55024: 1998, Amendment A2: 2003
9) Pick/Place, Soldering, Circuit Boards: IPC JSTD-001D, IPC-A-610D, ESD-STD-20.20, JESD-625a, IPC-A-610C Class 3
10) Printed Circuit Board (PCB): IPC-A-600G.
11) Connectors/Adapters/Cables: MIL-PRF-39012/55339, IPC JSTD-001D
12) Stainless Steel Material for Screws: DFARS 252-225-7014/DFARS 225.872-1, and MS Standards.
13) Aluminum Material: A16061-T6 per ASTM-B-221.
14) Chem Film: Mil-C-5541F Type I Class 1A for Yellow, Type II Class 1A for Clear.
15) Black Anodize: MIL-A-8625F Type II Class II.
16) REACH Compliance: SVHC Candidate List Published by European Chemical Agency (ECHA) on Oct-28-2008 Regarding Regulation (EC) No 1907/2006 Concerning REACH
17) CAGE Code: 3CVE1; ECCN: 5A991.b.4; HTS: 8529104000
18) Country of Origin: USA.
These commodities and technology are from the United States and exportable in accordance with the export
Administration regulations. Diversion contrary to U.S. law is prohibited.